GB320879A - Improvements in or relating to internal-combustion engines of the fixed radial cylinder type - Google Patents
Improvements in or relating to internal-combustion engines of the fixed radial cylinder typeInfo
- Publication number
- GB320879A GB320879A GB2135628A GB2135628A GB320879A GB 320879 A GB320879 A GB 320879A GB 2135628 A GB2135628 A GB 2135628A GB 2135628 A GB2135628 A GB 2135628A GB 320879 A GB320879 A GB 320879A
- Authority
- GB
- United Kingdom
- Prior art keywords
- casing
- fixed radial
- relating
- internal
- chamber
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M1/00—Carburettors with means for facilitating engine's starting or its idling below operational temperatures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B2075/1804—Number of cylinders
- F02B2075/1836—Number of cylinders nine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
- F02B75/222—Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/43—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
- F02M2700/4302—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air and fuel are sucked into the mixture conduit
- F02M2700/4392—Conduits, manifolds, as far as heating and cooling if not concerned; Arrangements for removing condensed fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
320,879. Fedden, A. H. R., Butler, L. F. G., and Bristol Aeroplane Co., Ltd. July 23, 1928. Cylinders, pipes for; crank chambers; pumps, centrifugal. -An annular induction chamber 11 is attached to a fixed radial-cylinder engine by extensions 17 of the usual bolts 15 connecting together the sections 13, 14 of the crank case. The engine is supported on a flanged conical plate 19 which is clamped to the crank case by the bolts 15. The chamber 11 may contain a stationary spiral distributor, or, as shown, it may form part of the casing of a rotary blower 23 which is mounted on an extension of the crank shaft 24. A casing 12 for engine accessories is attached to the casing of the chamber 11.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2135628A GB320879A (en) | 1928-07-23 | 1928-07-23 | Improvements in or relating to internal-combustion engines of the fixed radial cylinder type |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2135628A GB320879A (en) | 1928-07-23 | 1928-07-23 | Improvements in or relating to internal-combustion engines of the fixed radial cylinder type |
Publications (1)
Publication Number | Publication Date |
---|---|
GB320879A true GB320879A (en) | 1929-10-23 |
Family
ID=10161516
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2135628A Expired GB320879A (en) | 1928-07-23 | 1928-07-23 | Improvements in or relating to internal-combustion engines of the fixed radial cylinder type |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB320879A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2426877A (en) * | 1944-10-20 | 1947-09-02 | United Aircraft Corp | Radial aircraft engine |
-
1928
- 1928-07-23 GB GB2135628A patent/GB320879A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2426877A (en) * | 1944-10-20 | 1947-09-02 | United Aircraft Corp | Radial aircraft engine |
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